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API 663 2014 hairpintype heat exchangers

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Hairpin-type Heat Exchangers
API STANDARD 663
FIRST EDITION, MAY 2014
Special Notes
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guarantee in connection with this publication and hereby expressly disclaims any liability or responsibility for loss or
damage resulting from its use or for the violation of any authorities having jurisdiction with which this publication may
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Copyright © 2014 American Petroleum Institute
Foreword
Nothing contained in any API publication is to be construed as granting any right, by implication or otherwise, for the
manufacture, sale, or use of any method, apparatus, or product covered by letters patent. Neither should anything
contained in the publication be construed as insuring anyone against liability for infringement of letters patent.
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interpretation of the content of this publication or comments and questions concerning the procedures under which
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Suggested revisions are invited and should be submitted to the Standards Department, API, 1220 L Street, NW,
Washington, DC 20005, standards@api.org.
iii
Contents
Page
1
Scope . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
2
Normative References. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
3
Terms and Definitions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
4
General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3
5
Proposal Information Required . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4
6
6.1
6.2
6.3
Drawings and Other Required Data. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Outline Drawings and Other Supporting Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Information Required After Outline Drawings Are Reviewed. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Reports and Records . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
7
7.1
7.2
7.3
7.4
7.5
7.6
7.7
7.8
7.9
7.10
7.11
7.12
Design . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7
Design Temperature . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7
Design Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7
Cyclic Design . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8
Shell . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8
Front Closure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8
Rear Closure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10
Tube Bundle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10
Nozzles and Other Connections . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13
Shell Supports . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18
Gaskets . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18
Flanged External Girth Joints . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 18
Cladding for Corrosion Allowance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 19
8
8.1
8.2
8.3
8.4
Materials . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Requirements for Carbon Steel in Sour or Wet Hydrogen Sulfide Service . . . . . . . . . . . . . . . . . . . . . . . .
Gaskets . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Tubes. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
19
19
19
20
20
9
9.1
9.2
9.3
9.4
9.5
9.6
9.7
9.8
Fabrication . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Shells . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Tubes. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Welding . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Heat Treatment. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Dimensional Tolerances . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Gasket Contact Surfaces Other Than Nozzle Flange Facings . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Tube-to-Tubesheet Joints . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
20
20
20
21
21
22
22
22
23
10
10.1
10.2
10.3
10.4
Inspection and Testing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Quality Assurance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Quality Control. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Pressure Testing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Nameplates and Stampings . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
23
23
24
25
26
4
4
5
7
11 Preparation for Shipment . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 26
11.1 Protection . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 26
11.2 Identification . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 27
v
Contents
Page
12
12.1
12.2
12.3
Supplemental Requirements . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Design . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Examination . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
27
27
27
27
Annex A (informative) Recommended Practices . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 29
Annex B (informative) Hairpin Heat Exchanger Checklist . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 31
Annex C (informative) Hairpin Heat Exchanger Datasheets . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 33
Bibliography . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 44
Figures
1
Typical Components of a Hairpin Heat Exchanger . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2
2
Typical Front Closure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9
3
Typical Separated Head Front Closure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9
4
Typical Rear Closures . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10
5
Typical Impingement Sleeve . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12
6
Directions of Forces and Moments on Connections. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15
Tables
1
Minimum Wall Thickness of Tubes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2
Shell Side Nozzle Allowable Forces and Moments at Nozzle-to-Header Intersection
on the Shell Surface . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
3
Tube Side Nozzle Allowable Forces and Moments at the Face of the Terminal Connection . . . . . . . . . .
4
G Values for Tube Side Allowable Nozzle Load Calculation. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
5
Gasket Contact Surface Finishes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
6
Maximum Allowable Tube Wall Thickness Reduction for Roller-Expanded
Tube-to-Tubesheet Joints . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
7
Hardness Limits. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
B.1 Checklist for Hairpin Heat Exchangers. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
vi
11
15
15
17
22
23
24
31
Introduction
It is necessary that users of this standard be aware that further or differing requirements can be needed for
individual applications. This standard is not intended to inhibit a vendor from offering, or the purchaser from
accepting, alternative equipment or engineering solutions for the individual application. This can be particularly
applicable where there is an innovative or developing technology. Where an alternative is offered, it is the
responsibility of the vendor to identify any variations from this standard and provide details.
This standard requires the purchaser to specify certain details and features.
A bullet () at the beginning of a section or subsection indicates a requirement for the purchaser to make a
decision or provide information (for information, a checklist is provided in Annex B).
In this standard, where practical, U.S. Customary (USC) or other units are included in parentheses for information.
vii
Hairpin-type Heat Exchangers
1
Scope
This standard specifies requirements and gives recommendations for the mechanical design, materials
selection, fabrication, inspection, testing and preparation for shipment of hairpin heat exchangers for use
in the petroleum, petrochemical and natural gas industries. Hairpin heat exchangers include double-pipe
and multi-tube type heat exchangers.
2
Normative References
The following referenced documents are indispensable for the application of this document. For dated
references, only the edition cited applies. For undated references, the latest edition of the referenced
document (including any amendments) applies.
API Standard 521, Pressure-relieving and Depressuring Systems
ASME B16.5 1, Pipe Flanges and Flanged Fittings: NPS 1/2 through NPS 24 Metric/Inch Standard
NACE MR0103 2 , Materials Resistant to Sulfide Stress Cracking in Corrosive Petroleum Refining
Environments
NACE MR0175, Petroleum and natural gas industries—Materials for use in H2S containing environments
in oil and gas production—Parts 1, 2 and 3
NACE SP0472, Methods and Controls to Prevent In-Service Environmental Cracking of Carbon Steel
Weldments in Corrosive Petroleum Refining Environments
TEMA 3, Ninth Edition, Standards of the Tubular Exchanger Manufacturers Association
3
Terms and Definitions
For the purposes of this document, the following definitions apply.
3.1
cyclic service
Process operation with periodic variation in temperature, pressure and/or flowrate.
3.2
double-pipe
Single pipe within a shell.
3.3
effective heat transfer area
Outside surface area of the tubes that contributes to heat transfer including finned surface area (if any).
1
ASME International, 3 Park Avenue, New York, New York 10016-5990, www.asme.org.
2
NACE International (formerly the National Association of Corrosion Engineers), 1440 South Creek Drive,
Houston, Texas 77218-8340, www.nace.org.
3
Tubular Exchanger Manufacturers Association, 25 North Broadway, Tarrytown, New York 10591, www.tema.org.
1
2
API STANDARD 663
3.4
full-penetration weld
Welded joint that results in weld metal through the entire thickness of the components being joined.
3.5
front closure
Closure that connects the tube side to purchaser’s tube side piping and fixes the tube bundle or element
to the shell.
3.6
hairpin heat exchanger
Double-pipe (pipe-in-pipe) or multi-tube heat exchanger of two-leg bundle where each leg has its own
separate shell.
NOTE
Figure 1 shows typical components of a hairpin heat exchanger.
3.7
hairpin section
One U-tube element with two shell legs.
3.8
heat exchanger unit
One or more heat exchangers arranged in series or parallel for a specified service that work together to
perform the intended duty.
3.9
hydrogen service
Service that contains hydrogen at a partial pressure exceeding 700 kPa (100 psi) absolute.
3.10
item number
Purchaser’s identification number for a hairpin heat exchanger.
Key
1 shell
2 front closure
3 support
4
5
6
rear closure
tube side connection
shell side connection
Figure 1—Typical Components of a Hairpin Heat Exchanger
HAIRPIN-TYPE HEAT EXCHANGERS
3
3.11
minimum design metal temperature
Lowest metal temperature at which pressure-containing elements can be subjected to design pressure.
EXAMPLE
Ambient temperature or process fluid temperature.
3.12
multi-tube
Multiple tubes within a shell.
3.13
pressure design code
Recognized pressure vessel standard specified or agreed by the purchaser.
EXAMPLE
ASME BPVC, Section VIII; EN 13445 (all parts).
3.14
rear closure
Closure used at the return end of the heat exchanger which covers the U-bends.
3.15
sealing ring
Special gasket that provides a seal on the OD of tubesheet and the shell/tube side flange.
3.16
seal-welded
Tube-to-tubesheet joint weld of unspecified strength applied between the tubes and tubesheets for the
sole purpose of reducing the potential for leakage.
3.17
strength-welded
Tube-to-tubesheet joint welded so that the design strength is equal to, or greater than, the axial tube
strength specified by the pressure design code.
3.18
structural welding code
Recognized structural welding code specified or agreed by the purchaser.
3.19
tube bundle
Assembly of U-tubes, tube sheet and baffles.
4
General
 4.1 The pressure design code shall be specified or agreed by the purchaser. Pressure components
shall comply with the pressure design code and the supplemental requirements in this standard.
4.2 Where the use of TEMA is specified within this standard, the heat-exchanger construction shall
conform to TEMA, Class R, unless another TEMA class is specified.
4.3 Hairpin exchangers typically do not require expansion joints. However, it can be necessary to
evaluate some units to assess the requirement for an expansion joint. For such cases, the purchaser and
vendor shall agree to all relevant design, fabrication, inspection and testing requirements.
 4.4
The vendor shall comply with the applicable local regulations specified by the purchaser.
4
4.5
API STANDARD 663
Annex A includes recommended mechanical and design details for information.
4.6 Annex B provides a checklist that can be used by the purchaser to ensure that bulleted items in this
standard are addressed.
 4.7 The purchaser shall specify if the service is designated as sour in accordance with NACE MR0175
(all parts) for oil and gas production facilities and natural gas sweetening plants, or is designated as wet
hydrogen sulfide service in accordance with NACE MR0103 for other applications (e.g. petroleum
refineries, LNG plants and chemical plants), in which case all materials in contact with the process fluid
shall meet the requirements of the applicable standard to mitigate potential for sulfide stress cracking
(SSC). Identification of the complete set of materials, qualification, fabrication and testing specifications to
prevent in-service environmental cracking is the responsibility of the user (purchaser).
5
Proposal Information Required
5.1 For each heat exchanger unit, the vendor’s proposal shall include completed datasheets similar to
those appearing in Annex C.
5.2 For components that are not fully identified by Section 3, the vendor shall describe the details of
construction and assembly.
5.3 The proposal shall include a detailed description of all exceptions to the requirements of the
purchaser’s inquiry.
5.4 For stacked heat exchangers, the vendor shall supply the following components unless otherwise
specified by the purchaser:
a)
bolts, nuts, and gaskets for interconnecting nozzles;
b)
shims and bolting for interconnecting supports;
c)
external, interconnecting tube side piping.
5.5
6
6.1
The vendor shall supply a recommended spare parts list for each hairpin heat exchanger.
Drawings and Other Required Data
Outline Drawings and Other Supporting Data
6.1.1 The vendor shall submit, for review by the purchaser, outline drawings for each heat exchanger
unit. The drawings shall include the following information:
a)
service, item number, project name and location, purchaser’s order number, vendor’s shop order
number and other special identification numbers;
b)
design pressure, test pressure, maximum design temperature, minimum design metal temperature
and any restriction on testing or operation of the heat exchanger;
c)
maximum allowable working pressure (MAWP) in the corroded condition and at the design
temperature for the shell side and tube side;
d)
connection sizes, location, orientation, projection, direction of flow and, if flanged, the rating and
facing;
e)
coupling sizes, rating, and orientation;
HAIRPIN-TYPE HEAT EXCHANGERS
5
f)
dimensions, orientation and location of supports, including bolt holes and slots, and the stacking
arrangement;
g)
overall dimensions of the heat exchanger;
h)
tube bundle removal clearance;
i)
mass of the heat exchanger, empty and full of water, and of removable components with a mass
greater than 25 kg (60 lb), (e.g. removable tube bundle, individual front closure and rear closure);
j)
specified corrosion allowance for each side of the heat exchanger;
k)
references to the applicable code and the purchaser’s specification;
l)
requirements for postweld heat treatment;
m) requirements for NDE examination;
n)
requirements for material impact testing;
o)
requirements for surface preparation and painting;
p)
gasket materials;
q)
insulation thickness;
r)
location and orientation of nameplates, lifting lugs, grounding clips or other attachments;
s)
location of the center of gravity of the exchanger for empty and full of water;
t)
material specifications and grades for all components;
u)
forces and moments on connections, as specified by the purchaser;
v)
tube-to-tubesheet joint welding and testing procedures.
6.1.2 The vendor shall recommend the tools required for the assembly and maintenance of the hairpin
heat exchanger. If torquing of bolts is required, the vendor shall provide torquing procedures.
6.1.3 The review of engineering documents by the purchaser shall not relieve the vendor of the
responsibility of meeting the requirements of the purchase order.
6.2
Information Required After Outline Drawings Are Reviewed
6.2.1
Generic gasket information, including type and material, shall be provided.
6.2.2 Upon receipt of the purchaser’s review comments on the outline drawings, the vendor shall
submit copies of all detailed (nonproprietary) drawings. These shall fully describe the heat exchanger and
shall include at least the following information:
a)
full views and cross-sectional views, including tube bundle details with dimensions and materials;
b)
bundle details, including the following:
⎯
tube layout,
6
API STANDARD 663
⎯
number of baffles, type and description (for segmental baffles include cross-baffle cut, layout
and orientation in a view that shows the cut),
⎯
details and locations of all sealing and sliding strips;
c)
details of each pressure-retaining weld, including weld material, weld nominal thickness, weld
location, and applicable nondestructive examination method;
d)
details of each weld and weld nominal thickness for nonpressure attachments welded to pressure
parts and for all load bearing attachments;
e)
complete bills of materials, including the material specifications and part numbers for all proprietary
components;
f)
details of cladding and weld overlay;
g)
details of tube-to-tubesheet joints, including procedures for installation, welding, expansion,
inspection, and testing;
h)
flange-face finish.

6.2.3 If specified by the purchaser, the vendor shall furnish copies of applicable welding procedure
specifications, procedure qualifications and weld map for review or record.

6.2.4 The purchaser shall specify whether the vendor shall furnish for the purchaser’s review or record
the following documentation.
a)
Mechanical design calculations for shell thickness, tube thickness, nozzle reinforcement and other
nonproprietary pressure-retaining components. If calculations are made using computer software, all
input and output data shall be detailed so as to facilitate an understanding of the calculation
procedures. The equations in the applicable sections of the pressure design code and TEMA shall be
referenced.
b)
Minimum required thicknesses for all pressure-retaining components, whether they are proprietary or
nonproprietary.
c)
Maximum allowable working pressure (MAWP) calculations.
d)
Design calculations based on seismic, wind, transportation and/or piping loads, if these loads are
provided by the purchaser.
e)
Proposed procedures for assembly of flanged joints. Any required lubricants shall be stated.
f)
Design calculations for thermal loads imposed on nozzles of stacked heat exchangers.
g)
Flow-induced vibration analysis.
h)
Where sour or wet hydrogen sulfide service is specified, a Certified Material Test Report (CMTR)
shall be supplied in accordance with 8.2.2.
HAIRPIN-TYPE HEAT EXCHANGERS
6.3

7
Reports and Records
After the heat exchanger is completed, the vendor shall furnish the purchaser with the following
documents in the format and quantities specified by the purchaser:
a)
“as-built” datasheet;
b)
all outline and nonproprietary detail drawings, marked “CERTIFIED AS-BUILT”;
c)
certified record of all impact tests performed;
d)
certified mill test reports for all pressure-retaining parts, including tubes (each material test report
shall be identified by a part number);
e)
complete certified bill of materials suitable for obtaining all replacement parts, including quantity,
description, material specification and identification of each part;
f)
temperature charts of all postweld heat treatments;
g)
completed manufacturer’s data report in accordance with the pressure design code;
h)
nameplate rubbing or a facsimile;
i)
all as-built mechanical design calculations;
j)
nondestructive examination (NDE) map;
k)
all associated NDE reports, including radiographic, magnetic-particle, liquid-penetrant, ultrasonic,
hardness, impact, positive material identification (PMI) and any other reports as applicable;
l)
tube-wall reduction results;
m) tube-to-tubesheet leak-test results;
n)
hydrostatic test records in the form of a chart or certification;
o)
installation and maintenance instructions including lifting, handling and bundle removal.
7
Design
7.1

Design Temperature
7.1.1 All heat exchangers shall have two design temperatures for each side, a maximum design
temperature and a minimum design metal temperature (MDMT), as specified by the purchaser.
7.1.2 The design temperature of a component (including external bolting) influenced by both the shell
side and tube side fluids shall be the more severe design temperature.
7.2
Design Pressure
7.2.1 Unless otherwise specified or approved by the purchaser, the heat exchanger shall be designed
for design pressure on either side, with atmospheric pressure or, if specified, vacuum on the other side.
7.2.2 If the purchaser specifies that a calculation of maximum allowable working pressure (MAWP) is
required, there shall be no restrictions on what components can limit the MAWP of the hairpin heat
8
API STANDARD 663
exchanger. The MAWP shall be as defined in the applicable pressure design code and should be based
on all simultaneously existing external loads such as nozzle loads. The presence of external loadings
reduces the value of MAWP relative to the case where pressure is the only load present.
7.3
Cyclic Design

7.3.1

7.3.2 If cyclic service is specified, the purchaser shall specify the variation, the time for the variation
(hours, weeks, months, etc.) and the number of cycles or frequency for this variation expected during the
life of the equipment.

7.3.3
7.4
The purchaser shall specify if cyclic service design is required.
If cyclic service is specified, the purchaser shall define the type of analysis required.
Shell
7.4.1 The minimum thickness of the shell shall conform to TEMA, Class R, unless another TEMA class
is specified. For shell diameters smaller than those covered by TEMA, at least schedule 40 for carbon
steel and low-alloy steel and schedule 10 S for high alloy material shall be used.
7.4.2
7.5
Spiral welded pipe shall not be used.
Front Closure
7.5.1 Front closures are typically of a proprietary design utilizing either a common set of bolts (as
shown in Figure 2) or separate shell side and tube side bolting (as shown in Figure 3).
7.5.2
Separate shell side and tube side bolting shall be used in the following conditions:
a)
for services where the differential temperature (design or operating, whichever is greater) across the
tubesheets is greater than 220 °C (400 °F);
b)
design pressure for either side exceeds 7000 kPa (ga) (1000 psig);
c)
cyclic service;
d)
hydrogen service;
e)
when specified by the purchaser.
7.5.3 In units where the shell side and tube side share a common set of bolts, the design temperature
used for the bolting shall be the more severe of the shell side or tube side design temperature. For such
units, if the manufacturers design utilizes an intermediate or center flange with threaded bolt holes, this
center flange shall be designed for the more severe of the shell side or tube side design temperature, as
well as the higher of the shell side or tube side design pressure.
7.5.4
Corrosion allowances shall not be applied to split rings.
HAIRPIN-TYPE HEAT EXCHANGERS
Key
1 shell nozzle flange
2 tube nozzle flange
3 tube flange
4 shell end flange
5 tube bundle or element
6
7
8
9
10
9
shell pipe
closure bolting
tube gasket
sealing ring
shell closure split ring
NOTE
This is only one typical configuration. Other configurations are equally acceptable, e.g. the front closure can have
a concentric reducer, an eccentric reducer orientated flat-bottom or no reducer at all. Similarly, key item 2 can be absent
with the tube side connection being a simple butt-welded preparation. For nonremovable front closures, flanges, bolting and
gaskets are eliminated.
Figure 2—Typical Front Closure
Key
1 shell nozzle flange
2 tube nozzle flange
3 tube flange
4 shell end flange
5 tube bundle or element
6 shell pipe
7 closure bolting
8
9
10
11
12
13
14
tube gasket
sealing ring
shell closure split ring
tube closure split ring
compression flange
tube fitting flange
tube closure bolting
NOTE
This is only one typical configuration. Other configurations are equally acceptable, e.g. the front closure can have
a concentric reducer, an eccentric reducer orientated flat-bottom or no reducer at all. Similarly, key item 2 can be absent
with the joint being a simple butt-welded preparation. For nonremovable front closures, flanges, bolting and gaskets are
eliminated.
Figure 3—Typical Separated Head Front Closure
10
API STANDARD 663
7.6
Rear Closure
7.6.1
Two typical rear closure arrangements are shown in Figure 4.
a) Cast Closure
b) Fabricated Closure
Key
1
2
3
4
shell return bend housing
shell return housing assembly
shell return housing end flange
shell pipes
5
6
7
bundle or element assembly
return bend housing gasket
return bend housing bolting
NOTE
These are only two typical configurations for removable rear closures. Other configurations are equally
acceptable. For nonremovable rear closures flanges, bolting and gaskets are eliminated.
Figure 4—Typical Rear Closures
7.6.2 The minimum clearance between the tubes and the rear closure, under any of the specified
conditions, shall be 6 mm (1/4 in.).
7.6.3 For hydrogen, sour or wet hydrogen sulfide service, a confined gasket construction In accordance
with TEMA Clause R-6.5 shall be provided for the rear closure.
7.7
7.7.1
Tube Bundle
Tubes
7.7.1.1 The inner pipe or tube bundle of the heat exchanger shall be removable through the use of
bolted closure joints unless an all welded design is approved by the purchaser.
7.7.1.2 The minimum outside diameter of the tubes shall be 19.05 mm (3/4 in.), unless otherwise
specified or approved by the purchaser.
7.7.1.3 For tube bundles where the tube element is manufactured from tubing, the minimum tube-wall
thickness shall be as listed in Table 1, unless otherwise specified or approved by the purchaser.
HAIRPIN-TYPE HEAT EXCHANGERS
11
Table 1—Minimum Wall Thickness of Tubes
Dimensions in millimeters (inches)
Tube Material
Minimum Wall
Thickness a b
Carbon steel, low-alloy material (max. 9 % chromium), aluminum, and aluminum alloy
2.11 (0.083)
Copper and copper alloys
1.65 (0.065)
High-alloy [austenitic, ferritic, and austenitic/ferritic (duplex)] steel and other nonferrous
materials
1.473 (0.058)
Titanium
1.067 (0.042)
a
For low-fin tubing, this shall be the minimum thickness at the root diameter.
b
Average wall basis can be used provided the wall thickness is not less than that specified.
7.7.1.4 For tube bundles where the tube element is manufactured from pipe, the minimum wall
thickness shall be schedule 40 for carbon steel and low-alloy steel and schedule 5 S for high alloy
material.

7.7.1.5 The purchaser shall specify when a hairpin exchanger has been selected to mitigate a
complete tube rupture scenario, which would otherwise require a provision for pressure relief in
accordance with API 521. In such cases, the hairpin exchanger shall meet the following.
⎯ A double-pipe (pipe-in-pipe) configuration shall be used. A multi-tube hairpin type exchanger shall
not be permitted.
⎯ The inner element shall be made from pipe and shall be of the same schedule as, or thicker than, the
connecting pipe. The purchaser shall specify the connecting pipe schedule on the datasheet.
⎯ The minimum required wall thickness calculations for the inner pipe shall include the full hot and cold
side corrosion allowance, as specified on the datasheet.

7.7.1.6
The purchaser shall specify all maximum allowable lengths of straight tube due to plot
limitations, etc.
7.7.2
Transverse Segmental Baffles and Tube Supports
7.7.2.1 The thickness of segmental baffles and support plates shall be in accordance with TEMA.
Where the shell diameter is below 150 mm (6 in.), then the thickness for 150 mm (6 in.) diameter shells
shall be used.
7.7.2.2 Notched transverse baffles and support plates shall have notches that are 6 mm (1/4 in.) high to
facilitate drainage for shell diameters up to and including 406 mm (16 in.). Above this diameter, notches
shall be 10 mm (3/8 in.) high.
7.7.2.3
7.7.3
Maximum baffle spacing for bare and low-fin tubes shall be in accordance with TEMA.
Impingement Protection
7.7.3.1 If required by TEMA standards (RCB-4.61), impingement protection shall be provided by
impingement sleeves, plate or rods on the tube bundle, a distributor belt, or another means agreed upon
by the purchaser and the vendor. A typical impingement sleeve is shown in Figure 5.
12
API STANDARD 663
Key
1 shell side nozzle
a
2 impingement sleeve
3 tubes
4 first baffle
a
The impingement sleeve should be welded to the first baffle.
Figure 5—Typical Impingement Sleeve
7.7.3.2
If an impingement plate is used:
a)
it shall extend at least 25 mm (1 in.) beyond the projection of the nozzle bore, unless otherwise
agreed with purchaser;
b)
the nominal thickness of impingement plates from carbon steel or low-alloy steel shall be not less
than 6 mm (1/4 in.), unless otherwise agreed with purchaser;
c)
the impingement plate shall be adequately supported, e.g. by welding to at least two spacers, to
avoid mechanical damage due to vibration;
d)
it shall not be perforated.
7.7.3.3 Impingement protection shall be provided on both legs to allow for bundle rotation, except in
shell side vaporizing service.
7.7.3.4 The rho-V-squared values at the shell and bundle entrance and exit areas shall not exceed the
limits specified by TEMA Standards.
7.7.4
Bundle Skid Bars
7.7.4.1 For all removable bundles with a mass of more than 5500 kg (12,000 lb), a continuous sliding
surface shall be provided to facilitate bundle removal. If skid bars are used, they shall be welded to the
transverse baffles and supports to form a continuous sliding surface.
7.7.4.2 Skid bars shall protrude at least 1 mm (1/32 in.) beyond the outside diameter of baffle and
supports.
HAIRPIN-TYPE HEAT EXCHANGERS
13
7.7.4.3 The leading and trailing edges of skid bars shall be provided with a radius or a bevel to prevent
damage to the shell when inserting or removing the bundle.
7.7.4.4 Provision shall be included to protect tubesheet sealing surface from damage during bundle
insertion or removal.
7.7.5
Tube-to-Tubesheet Joint
The tube-to-tubesheet joint shall be in accordance with the TEMA standard, unless otherwise specified by
the purchaser.
7.8
Nozzles and Other Connections
7.8.1 Flanges shall be in accordance with the pressure design code, unless otherwise specified by
purchaser.
7.8.2 Connections DN 40 (NPS 1-1/2) and larger shall be flanged, unless otherwise specified by the
purchaser.
7.8.3 Connection sizes of DN 32 (NPS 1-1/4), DN 65 (NPS 2-1/2), DN 90 (NPS 3-1/2) or DN 125
(NPS 5) shall not be used.
7.8.4
If welded connections are specified, they shall be beveled.
7.8.5 Non-flanged connections smaller than DN 40 (NPS 1-1/2) shall be forged couplings with an
appropriate rating, for example, equivalent to ASME B16.11 class 6000, or shall be integrally reinforced
welding fittings with appropriate tapered threads, for example, equivalent to ASME B1.20.1, and shall
comply with the pressure design code. Threaded connections shall not be used in hydrogen, sour or wet
hydrogen sulfide service. This includes auxiliary connections such as vents, drains, instrument
connections and chemical cleaning connections.
7.8.6
Flanged connections shall be of one of the following types:
a)
forged integrally flanged;
b)
pipe or forged cylinder welded to forged welding-neck flange;
c)
pipe welded to a forged slip-on flange, except as noted in 7.8.7.
7.8.7
Slip-on flanges shall not be used in any of the following conditions:
a)
for design pressure exceeding 2100 kPa (ga) (300 psig);
b)
for design temperature exceeding 400 °C (750 °F);
c)
for corrosion allowance exceeding 3 mm (1/8 in.);
d)
in hydrogen service, sour, or wet hydrogen sulfide service;
e)
in cyclic service.
 7.8.8 When specified by the purchaser, the projection of flanged connections shall allow the removal of
through-bolting from either side of the flange without removing the insulation. This requirement does not
14
API STANDARD 663
apply to the interconnecting nozzles of stacked units. The insulation thickness shall be specified by the
purchaser.
7.8.9 Integrally reinforced nozzles shall be designed so that standard spanners (wrenches) fit the nuts
without interference from nozzle neck reinforcement.
7.8.10 All bolt holes for flanged or studded connections shall straddle centerlines.
 7.8.11 The purchaser shall specify if chemical cleaning connections are required. Their nominal size
shall be not less than DN 50 (NPS 2). Chemical cleaning connections shall not be utilized on the tube
side of exchangers.
7.8.12 Each nozzle as defined in 7.8.14, in its corroded condition, shall be capable of withstanding the
simultaneous application of the moments and forces listed in Table 2 and Table 3, unless otherwise
specified by the purchaser.
7.8.13 The points of application and directions of the forces and moments are shown in Figure 6. These
moments and forces shall be the total from all sources, including dead loads and thermal loads.
7.8.14 The nozzle moments and forces listed in Table 2 and Table 3 shall be used for hairpin
exchangers. The tables are based on the following criteria.
a)
The support closest to the shell nozzles is fixed.
b)
Shell material is carbon steel.
c)
Shell side design pressure does not exceed 60 % of the maximum allowable pressure of the
corroded shell, calculated for internal pressure only.
d)
Shell side design temperature does not exceed 350 °C (650 °F).
e)
Shell diameter is at least one size bigger than the nozzle size.
f)
Nominal shell thickness is at least standard weight pipe wall thickness.
g)
Minimum corroded shell thickness is not less than 2.5 mm (3/32 in.).
h)
Shell corrosion allowance is not greater than 3 mm (1/8 in.).
i)
Minimum nozzle thickness is at least schedule 160 for nominal nozzle sizes up to 50 mm (2 in.) and
schedule 80 for nominal nozzle sizes 80 mm (3 in.) and above.
j)
There shall be no additional connections fitted on the tube side nozzle reducers that will extend the
typical location of the terminal connection from the front closures, as shown in Figure 2 and Figure 3.
k)
Front closures are adequately overdesigned with extra equivalent pressure above the design
pressures to allow room for the tube side nozzle loads.
l)
The exchanger is a single, nonstacked unit and is not exposed to wind, seismic or motion loads.
HAIRPIN-TYPE HEAT EXCHANGERS
15
NOTE 1
Force vector “X” is in the direction of the heat exchanger’s centerline.
NOTE 2
“●” indicates the point of application for the forces and moments on the connection.
Figure 6—Directions of Forces and Moments on Connections
Table 2—Shell Side Nozzle Allowable Forces and Moments at Nozzle-to-Header
Intersection on the Shell Surface
Nominal
Diameter
My
Mx
Mz
Fx
Fy
Fz
DN
(NPS)
N⋅m
(lbf⋅ft)
N⋅m
(lbf⋅ft)
N⋅m
(lbf⋅ft)
N
(lbf)
N
(lbf)
N
(lbf)
50
2
115
85
115
85
115
85
266
60
266
60
266
60
80
3
135
100
135
100
135
100
333
75
333
75
333
75
100
4
237
175
237
175
237
175
667
150
667
150
667
150
150
6
372
275
372
275
372
275
1000
225
1000
225
1000
225
200
8
542
400
542
400
542
400
1556
350
1556
350
1556
350
250
10
745
550
745
550
745
550
2001
450
2001
450
2001
450
300
12
1172
865
1172
865
1172
865
2313
520
2313
520
2313
520
Table 3—Tube Side Nozzle Allowable Forces and Moments at the Face of the Terminal Connection
Nominal
Diameter
My
Mx
Mz
Fx
Fy
Fz
DN
(NPS)
N⋅m
(lbf⋅ft)
N⋅m
(lbf⋅ft)
N⋅m
(lbf⋅ft)
N
(lbf)
N
(lbf)
N
(lbf)
50
2
79
59
79
59
79
59
186
42
186
42
186
42
80
3
94
70
94
70
94
70
231
52
231
52
231
52
100
4
165
122
165
122
165
122
467
105
467
105
467
105
150
6
260
192
260
192
260
192
698
157
698
157
698
157
200
8
379
280
379
280
379
280
1089
245
1089
245
1089
245
250
10
521
385
521
385
521
385
1401
315
1401
315
1401
315
300
12
820
605
820
605
820
605
1619
364
1619
364
1619
364
16
API STANDARD 663
NOTE
Forces (F) and moments (M) shown in Table 2 and Table 3 were determined as follows.
a)
For each nozzle size, the same maximum values for forces and moments in all three directions,
i.e. Fx = Fy = Fz, and Mx = My = Mz were adopted.
b)
The worst-case assumptions were made, as listed above, in the criteria to allow the application of the table
values to a wide range of exchanger parameters.
c)
These assumed exchangers were analyzed as a whole system, considering the general stresses in the shell,
local stresses in the nozzle-to-shell junction, front end closure integrity, support stresses, and anchor bolt
stresses to determine the weakest link.
7.8.15 The nozzle-to-shell junction shall be analyzed using WRC 537 or finite element analysis (FEA)
with the pressure thrust load applied simultaneously with the nozzle loads listed in Table 2. In addition,
the effect of tube side nozzle loads shall be investigated and accounted for at the nozzle-to-shell junction.
7.8.16 Front closures shall be designed to withstand the tube side nozzle loads shown in Table 3 using
the equivalent pressure, Pe, expressed in kilopascals (gauge) as calculated by Equation (1) for SI units or
expressed in pounds per square inch (gauge) as calculated by Equation (2) for USC units:
In SI units:
(
)  +  ( 4000 × F )  + P
)   (π × G ) 
 16 × 10 6 × M
Pe = 

π ×G3

(
(1)
2
In USC units:

 
(192 × M )  +  ( 4 × F )
Pe = 
3  
2
 π × G
  π × G
(
)
(
)

+P


(2)
where
M
is the bending moment (vector quantity), expressed in N ⋅ m (lbf ft); see Equation (4) or (5);
F
is the force (vector quantity), expressed in N (lbf); see Equation (3);
G
is the gasket reaction diameter, expressed in mm (in.); see Table 4;
P
is the design pressure, expressed in kPa (ga) (psig).
F = Fx
(3)
In SI units:
1
2
2

 2
M =   M y + Fx × 10 −3 × d z + Fz × 10 −3 × d x  +  M z + Fx × 10 −3 × d y + Fy × 10 −3 × d x  



 
 
(
) (
)
(
) (
)
(4)
HAIRPIN-TYPE HEAT EXCHANGERS
17
In USC units:
2
2


dy  

dz  
d x 
d x  


M =   M y +  Fx ×
 +  Fy ×
 +  Fz ×
  +  M z +  Fx ×
 
12  
12  
12  
12   






1
2
(5)
where
Fx, Fy and Fz
are the nozzle forces on each axis, as diagrammed in Figure 6;
Mx, My and Mz
are the nozzle moments acting about each axis, as diagrammed in Figure 6;
dx, dy and dz
are the distances between the point of application of the forces / moments and the
center of the gasketed joints (shell or tube side closure joint) being analyzed in the
x, y, and z directions, respectively, as shown in Figure 6, expressed in millimeters
(inches).
In addition, the bolting of the front closure shall be designed to withstand the shear force, V, expressed in
newtons, as calculated in Equation (6) or expressed in pounds-force as calculated in Equation (7):
In SI units:
V = ( Fy 2 + Fz 2 )
1
2
 2 × 10 3 × M
x
+

D
BC

1
2
 24 × M x 
+

 DBC 




(6)
In USC units:
V = ( Fy 2 + Fz 2 )
(7)
where
DBC
is the bolt circle diameter of the closure being analyzed, expressed in millimeters (inches).
Table 4—G Values for Tube Side Allowable Nozzle Load Calculation
Nominal Shell
Diameter
G
Separated Bolting
Closure
DN
(NPS)
mm
(in.)
50
2
33
1.3
80
3
56
2.2
100
4
84
3.3
125
5
107
4.2
150
6
135
5.3
200
8
183
7.2
250
10
230
9.1
300
12
275
10.8
Common Bolting
Closure
mm (in.)
(Use nominal
pipe size)
18
API STANDARD 663
7.8.17 The equivalent pressure uses the tube side closure flange gasket mean diameter for the separate
bolting head closure, or the shell side closure flange gasket mean diameter for the common bolting head
closure as G in the calculation (Table 4). The calculated equivalent pressure, Pe, shall be equal to or less
than the MAWP of each front closure and the center flange on the common head closure type. It is
necessary that all three forces and moments acting on the nozzle be accounted for.
7.8.18 Shell side and tube side nozzle flanges in high temperature service [above 200 °C (400 °F) for
ASME B16.5 Class 150 flanges, or above 400 °C (750 °F) for ASME B16.5 Class 300 and higher flanges]
shall be checked using the following procedure.
Calculate the equivalent pressure, Pe, for G, the gasket reaction diameter, corresponding to the nozzle
flange, using Equation (1) or Equation (2) for SI or USC units, respectively.
If the calculated Pe is equal to or less than the rated pressure of the nozzle flange in accordance with
ASME B16.5, the selected flange is acceptable; otherwise, use the next higher flange pressure class.
7.8.19 The heat exchanger shall be drainable and ventable through the connections for all pass
arrangements. Eccentric reducers can be used to provide for this.
7.9
Shell Supports
7.9.1 Both legs of the exchanger’s shell shall be fixed at the support closest to the tubesheet, unless
otherwise specified by the purchaser.
7.9.2 When the fixed shell support of a removable-bundle heat exchanger is fixed to the shell, it shall
be designed to withstand a longitudinal force equal to 150 % of the bundle mass applied at the heat
exchanger bundle centerline. The shear stress for supports shall not exceed 40 % of the yield strength of
the material.
7.9.3
shell.
Support material in direct contact with the shell shall be of the same nominal composition as the
7.9.4 The lower shells of stacked removable-bundle heat exchangers shall be designed to carry the
superimposed loads without suffering distortion that can cause binding of the tube bundles.
7.9.5
All units shall have at least one earthing lug, welded directly to a suitable shell side component.
7.10 Gaskets
7.10.1 Spiral-wound gaskets, where used, shall be provided with a means to prevent over-compression
and buckling.
7.10.2 Gaskets shall be of a one-piece design. Gaskets made integral by welding are acceptable.
Circular gaskets shall have no more than two welds. Obround gaskets shall have no more than four welds.
7.11 Flanged External Girth Joints
7.11.1 External girth joints shall be of through-bolted construction, unless otherwise approved by the
purchaser.
7.11.2 Minimum bolt diameter shall be 12 mm (1/2 in.).
7.11.3 Slip-on flanges shall not be used as girth flanges.
HAIRPIN-TYPE HEAT EXCHANGERS
19
7.11.4 The gap between mating flanges after assembly shall be not less than 3 mm (1/8 in.) and this gap
shall extend within the bolt circle to allow checking the flanges for radial distortion caused by an
excessive bolt load.
7.11.5 Through-hardened washers shall be provided under nuts for all bolts having a diameter of 38 mm
(11/2 in.) or larger unless hydraulic bolt tensioners are used. The washers shall be at least 6 mm (1/4 in.)
thick.

7.11.6 The purchaser shall specify if bolt-tightening devices will be used. When used, the nozzles and/or
girth flanges shall be designed to allow adequate clearance.
7.12 Cladding for Corrosion Allowance
7.12.1 If cladding (including weld overlay) is used, the cladding thickness shall be used only as a
corrosion allowance and not for pressure design.
7.12.2 The cladding thickness at the tube side face of a tubesheet shall be not less than 10 mm (3/8 in.)
when tubes are expanded only, and 5 mm (3/16 in.) when tubes are welded to the tubesheet. If grooves
are used, the first groove shall be within the tube side cladding.
7.12.3 The cladding thickness on the shell side face of a tubesheet shall not be less than 10 mm (3/8 in.).
7.12.4 Weld overlays shall have sufficient thickness to provide the specified chemical composition to a
depth of at least 1.5 mm (1/16 in.).
8
Materials
8.1
8.1.1
General
Cast steel can be used only for the return bend housing.
8.1.2 Material for external parts that are welded directly to the heat exchanger, such as pads, brackets
and lugs, shall be of the same nominal composition as the material to which they are welded.
8.1.3 If alloy linings are specified by the purchaser, they shall be weld-overlay, integrally clad or
explosion-bonded. Loose liners or sleeves shall not be used without the approval of the purchaser.
8.1.4
Girth flanges can be fabricated from forgings or plate.
8.1.5
Shells and nozzles can be welded pipe, seamless pipe or rolled and welded cylinders.
8.1.6 Shell supports shall be fabricated using structural grade carbon steel unless otherwise specified
by the purchaser.
8.2
Requirements for Carbon Steel in Sour or Wet Hydrogen Sulfide Service
8.2.1 Materials shall be supplied in the normalized condition, unless otherwise approved by the
purchaser. The acceptability of hot-formed material shall be subject to approval of the purchaser.
8.2.2 Pressure-retaining components and internals welded to pressure-retaining components shall be
supplied with a Certified Material Test Report (CMTR). The CMTR shall include the unspecified elements
chromium (Cr), columbium (Cb) [also known as niobium (Nb)], nickel (Ni), vanadium (V), molybdenum
(Mo) and copper (Cu) that are used in the equation to calculate the carbon equivalent (CE), as defined by
NACE MR0175 (all parts) or NACE MR0103.
20
API STANDARD 663
 8.2.3 The maximum allowable carbon equivalent shall be agreed to with the purchaser, prior to
purchase of materials for use in fabrication. Restrictions on other residual elements and micro-alloying
elements can also apply, depending on the severity of the service. The purchaser shall specify any such
restrictions.
8.3
Gaskets
Gaskets shall not contain asbestos.
8.3.1
8.3.2 Material for metal-jacketed, serrated-metal or solid-metal gaskets shall have a corrosion
resistance at least equal to that of the gasket contact surface material.
8.3.3 Metal windings of spiral-wound gaskets shall be of austenitic stainless steel, unless otherwise
specified or approved by the purchaser. Where materials of construction are a higher alloy, then the metal
windings shall be the same alloy material.
8.3.4 Serrated or solid-metal gaskets, including welds, shall be softer than the gasket contact surface,
except that for special, high-pressure, closure designs (e.g. self-energizing types), the sealing ring may
be harder than the gasket contact surfaces.
8.3.5 Gasket material, including filler material, shall be selected to withstand the maximum design
temperature.
8.3.6 Compressed sheet type gaskets shall not be used in hydrocarbon, steam, hydrogen, sour or wet
hydrogen sulfide service.
8.4
Tubes
8.4.1 Integrally finned tubes of copper alloy shall be furnished in the annealed-temper condition, such
as ASTM B359/B359M.
All welded tubes in the finished condition shall be eddy-current tested over their full length.
8.4.2
9
Fabrication
9.1
Shells
9.1.1 For removable heat exchanger bundles, all longitudinal and circumferential shell welds shall be
finished flush with the inner contoured for ease of tube-bundle insertion and withdrawal.
9.1.2 For removable-bundle heat exchangers, the permissible out-of-roundness of a completed shell,
after any required heat treatment, shall allow the tubesheets and baffles or tube supports to pass through
the entire shell length without binding.
9.2
Tubes
9.2.1
General
Tube elements shall be fabricated from either tubing or pipe material.
9.2.2
Elements Made from Tubing
9.2.2.1 All plain and low-finned tubes, including U-tubes, shall be formed from a single length and shall
have no circumferential welds, unless approved by the purchaser.
9.2.2.2
Tubes with longitudinal fins can have circumferential welds at the bend area.
HAIRPIN-TYPE HEAT EXCHANGERS
21
9.2.2.3 Tube thickness after bending and forming shall not be less than the minimum thickness
required by the pressure design code. Out-of-roundness of the bent portion shall not be greater than
10 % of the tube outside diameter.
9.2.2.4 When not specified by the pressure design code, the minimum tube thickness after bending
and forming shall be in accordance with the requirements of TEMA Paragraph RCB-2.31.
9.2.3
Elements Made from Pipe
U-bends can be fabricated with circumferential welds using pipe and/or butt weld fittings.
9.3
9.3.1
Welding
Welds can be made by any welding process other than oxyacetylene gas welding.
9.3.2 Pressure-retaining welded joints shall be full-penetration weld type, except where slip-on flanges
are allowed in accordance with 7.8.
9.3.3
Where slip-on flanges are used, they shall be welded from both sides.
9.3.4 Openings in plate components, to which attachments abut the openings, shall be inspected for
laminations. The surface of the opening through the plate shall be examined by means of the
magnetic-particle, liquid-penetrant or ultrasonic methods. Subject to agreement with the purchaser,
indications found shall be cleared to sound metal and then repair-welded.
9.3.5
Permanent backing strips shall not be used.
9.3.6 All strength-welded tube-to-tubesheet welds shall be produced by gas tungsten arc, using filler
material.
9.3.7 Welds attaching nonpressure external attachments (such as lugs or structural steel supports)
shall be continuous, except for insulation support rings.
9.3.8 Repair-associated welding procedures shall be submitted to the purchaser for approval before the
start of repair.
9.3.9
Longitudinal fins shall be attached by electric resistance welding. Stitch welding is not acceptable.
 9.3.10 The purchaser shall specify whether weld procedure qualifications for carbon steel in sour or wet
hydrogen sulfide service, including tube to tubesheet welds, shall include a micro-hardness survey
performed on a weld cross-section and transverse to the weld centerline. The micro-hardness testing and
acceptance criteria shall be in accordance with NACE SP0472 or NACE MR0175 (all parts), as
applicable. Any additional restrictions on residual elements or micro-alloying elements for the qualification
test material shall be specified by the purchaser.
9.4
Heat Treatment
9.4.1 Machined contact surfaces, including any threaded connections, shall be suitably protected to
prevent scaling or loss of finish during heat treatment.
 9.4.2 Requirements for heat treatment after bending for the bend portion of U-tubes shall be specified
by the purchaser. The procedure shall be agreed to between purchaser and vendor.
9.4.3
point.
The heat-treated portion of the U-bend shall extend at least 150 mm (6 in.) beyond the tangent
22
API STANDARD 663
 9.4.4
The purchaser shall specify if heat treatment is required for process reasons.
 9.4.5
The purchaser shall specify if postweld heat treatment is required for weld-overlaid components.
9.4.6 For sour and wet hydrogen sulfide service, the minimum postweld heat treatment requirements
for carbon steel construction shall be in accordance with NACE SP0472. The minimum hold time shall be
in accordance with the pressure design code, or 1 h, whichever is greater.
9.5
Dimensional Tolerances
9.5.1
Manufacturing tolerances shall be in accordance with TEMA, except as noted in this standard.
9.5.2 Heat exchangers that will be stacked in series shall be stacked in the shop to check for proper
connection alignment.
9.5.3 For stacked heat exchangers, mating nozzle flanges shall not be out-of-parallel with each other
by more than 1 mm (1/32 in.), measured across any diameter. The clearance between mating nozzle
flanges shall not exceed 3 mm (1/8 in.) after gasket assembly and installation. Bolts shall be capable of
being inserted and removed freely without binding. Shims shall be installed, as required, between the
supports and shall be tack-welded in place.
9.6
Gasket Contact Surfaces Other Than Nozzle Flange Facings
9.6.1
Gasket contact surfaces shall have the finishes shown in Table 5.
Table 5—Gasket Contact Surface Finishes
Dimensions in micrometers (micro-inches).
Type
Solid metal gaskets
Double jacketed gaskets
Surface Roughness
Raa
1.6 (63) maximum
1.6 to 3.2 (63 to 125)
Spiral-wound gaskets
3.2 to 6.3 (125 to 250)
Serrated or corrugated metal gaskets with soft gasket-seal facing
Compressed sheet gaskets
a
3.2 to 12.5 (125 to 500)
Ra is roughness average and is expressed in μm (μin).
9.6.2
The flatness tolerances on peripheral gasket contact surfaces shall be in accordance with TEMA.
9.6.3 Flange flatness tolerance and surface finish shall be measured after the flange has been attached
to the component cylinder or the cover and after any postweld heat treatment.
9.6.4 The flatness of tubesheet gasket-contact surfaces shall be measured after the tube-to-tubesheet
joints have been completed, including any heat treatment.
9.7
9.7.1
Tube-to-Tubesheet Joints
Tube-hole grooves shall be square-edged, concentric and free from burrs.
HAIRPIN-TYPE HEAT EXCHANGERS
23
9.7.2 If austenitic stainless steel, duplex stainless steel, titanium, cupro-nickel or nickel-alloy tubes are
specified, the tube holes shall be machined in accordance with TEMA, Table RCB-7.41, column (b)
(Special Close Fit).
9.7.3 Strength-welded joints shall be used when tube hole ligaments are less than those required by
TEMA. Tubes shall be given a light contact roll after welding.
9.7.4
Recessed tube-to-tube sheet welds are not acceptable, unless agreed with purchaser.
9.7.5 If roller-expanded joints are utilized, the tube wall thickness reduction shall be in accordance with
Table 6. For multi-tube exchangers, a minimum of 2 % of the tubes per tube bundle, with a minimum of
3 tubes, shall be randomly checked for conformance to this requirement.
Table 6—Maximum Allowable Tube Wall Thickness Reduction for
Roller-Expanded Tube-to-Tubesheet Joints
Material
Maximum Tube Wall Thickness Reduction
%
Carbon steel and low-alloy (max. 9 % chromium) steel
8a
Stainless and high alloy steel
6a
Titanium and work hardening nonferrous
5a
Non-ferrous non-work hardening (e.g. admiralty brass)
8a
a
These can be increased by a further 2 %, if approved by the purchaser.
9.7.6 If welded-and-expanded joints are specified, tube wall thickness reduction should begin at least
6 mm (1/4 in.) away from welds.
9.7.7
In no case shall the rolling encroach within 3 mm (1/8 in.) of the shell side face of the tubesheet.
9.7.8 For shell-side-clad tubesheets, the tube(s) shall be expanded to seal against the cladding
material, for a minimum distance of 6 mm (1/4 in.).
9.8
Assembly
9.8.1 The threads of external studs and nuts shall be coated with a suitable anti-seize compound to
prevent galling.
9.8.2 The lifting device shall be a weld-on lug or ring provided with a hole not less than 25 mm (1 in.) in
diameter. Wherever possible, the lug or ring shall be located at the top of the component, above its center
of gravity; otherwise, two suitably located lugs or rings shall be provided. The lifting device shall be
designed to support at least twice the mass of the component.
10 Inspection and Testing
10.1
Quality Assurance
 10.1.1 The purchaser shall specify if the vendor is required to supply information about its quality control
system and if this includes submission of a quality control plan.
10.1.2 No tubes or tube holes shall be plugged without notifying the purchaser. The method and
procedure of plugging shall be subject to approval by the purchaser.
24
API STANDARD 663
10.2
Quality Control
10.2.1 For external pressure containing welds, the following requirements apply.
a)
At least one radiograph shall be made of each butt welded joint. Nozzle welds are exempt from this
requirement, unless required by the pressure design code. The radiographs shall be at least 250 mm
(10 in.) long, or shall be full length if the weld is less than 250 mm (10 in.) long.
b)
Weld porosity limits for radiographs shall be as stated in the pressure design code for fully
radiographed joints.
10.2.2 A minimum of 10 % of the circumferential joints of tubes or inner pipes shall be fully radiographed.
 10.2.3 When specified by the purchaser, weld metal of pressure-retaining welds (excluding tube to
tubesheet welds) in carbon steel components shall be hardness tested.
10.2.4 Carbon steel welds in cyclic, sour or wet hydrogen sulfide services shall be hardness tested.
10.2.5 Weld metal of pressure-retaining welds (excluding tube-to-tubesheet welds) in components made
of Cr-Mo, 11/13/17 % chromium steels and duplex stainless steels shall be hardness tested.
10.2.6 Weld hardness testing of each hairpin section shall be as follows.
a)
One longitudinal weld, one circumferential weld and each connection-to-component weld if the
connection is DN 50 (NPS 2) or larger, shall be examined.
b)
Examination shall be made after any required postweld heat treatment.
c)
Unless otherwise agreed between the vendor and purchaser, the weld hardness shall not exceed the
values listed in Table 7.
d)
Hardness readings shall be taken with a portable Brinell hardness tester. Other hardness testing
techniques may be employed if approved by the purchaser. When access is available, tests shall be
performed on the side of the weld in contact with the process fluid.
e)
If more than one welding procedure is used to fabricate longitudinal or circumferential welds,
hardness readings shall be made of welds deposited by each procedure.
f)
Hardness test results and locations shall be recorded.
Table 7—Hardness Limits
Material
Maximum Weld Hardness
Carbon steel
225 HBW
Chromium steel (up to 3 % Cr)
225 HBW
Chromium steel (5 % Cr to 17 % Cr)
241 HBW
Duplex stainless steel (22 % Cr)
to be agreed with purchaser
Super duplex stainless steel (25 % Cr)
to be agreed with purchaser
NOTE
These hardness values are for general services. More stringent hardness testing and acceptance
criteria can be required for special services (e.g. sulfide stress cracking or other types of environmental
cracking services, as specified in NACE Standards).
HAIRPIN-TYPE HEAT EXCHANGERS
25
10.2.7 At welded joints in alloy-clad construction, the weld in the base metal and the area adjacent to the
weld where the cladding has been stripped back shall be examined by magnetic-particle inspection
before weld overlay of the joint.
10.2.8 All finished welds in ferromagnetic steel shall be examined after postweld heat treatment (unless
the pressure design code specifies examination after hydrostatic testing) by the magnetic particle method.
10.2.9 For carbon steel and low-alloy steels in sour or wet hydrogen sulfide service, all accessible
wetted surfaces of pressure-retaining welds and attachment welds to the pressure boundary shall be
examined by the wet fluorescent magnetic particle method after postweld heat treatment. Liquid penetrant
examination shall be substituted for those welds that cannot otherwise be examined by magnetic particle
methods.
10.2.10 Final welds in all nonmagnetic materials, whether of solid alloy or alloy-clad plate, shall be
examined by the liquid-penetrant method after any required postweld heat treatment.
10.2.11 After cladding, but prior to fabrication, integrally clad material shall be subjected to an ultrasonic
examination from the clad side in accordance with the pressure design code.
10.2.12 Overlay weldments, back-cladding and attachment welds to overlay weldments shall be
liquid-penetrant examined after postweld heat treatment.
10.2.13 For duplex stainless steels, the ferrite content of all accessible completed production welds shall
be checked using a ferrite-scope. A minimum of three tests shall be made on each 1.5 m (5 ft) of weld,
with at least three tests made on each longitudinal seam, three tests on each circumferential weld seam
and three tests on each nozzle weld. The acceptance criteria for the minimum and maximum ferrite
content shall be agreed between the purchaser and vendor.

10.2.14 The purchaser shall specify whether all carbon steel plate in sour or wet hydrogen sulfide service
shall be subjected to an ultrasonic lamination check (e.g. to EN 10160 grade S2E2 or ASME SA-578,
acceptance level A supplementary requirement S1).
10.3
Pressure Testing
10.3.1 The design of the heat exchanger shall permit full hydrostatic testing on the shell side with the
tube side closure components removed, either through use of a threaded center flange, a test ring or
alternate means. The shell-side hydrostatic test shall be conducted with the front closure removed.
10.3.2 In the case of welded-and-expanded tube-to-tubesheet joints, the tube weld integrity shall be
verified before expansion of the tubes by a pneumatic test from the shell side at a gauge pressure of
between 50 kPa (7.5 psi) and 100 kPa (15 psi), using a soap-water solution to identify leaks.
10.3.3 Except for differential-pressure designs, an independent hydrostatic test of the shell side and the
tube side shall be performed. The minimum fluid temperature for hydrostatic testing shall be as required
by the pressure design code.
10.3.4 The water used for hydrostatic testing shall be potable and the test pressure shall be maintained
for at least 1 h.
10.3.5 The chloride content of the test water used for equipment with austenitic stainless steel materials
that can be exposed to the test fluid shall not exceed 50 mg/kg (50 parts per million by mass). Upon
completion of the hydrostatic test, the equipment shall be promptly drained and cleared of residual test
fluid.

10.3.6 Any additional requirements for equipment drying or preservation shall be specified by the
purchaser.
26
API STANDARD 663
10.3.7 Nozzle reinforcement pads shall be pneumatically tested between 100 kPa (ga) (15 psig) and
170 kPa (ga) (25 psig).
10.3.8 Joints taken apart after the final pressure test shall be reassembled with new gaskets. Selfenergizing seals can be reused subject to approval of the purchaser.
10.3.9 Paint or other external coatings shall not be applied over welds before the final hydrostatic test
unless otherwise agreed by the purchaser.
10.3.10 Heat exchangers that will be stacked in service shall be hydrotested stacked.
10.4
Nameplates and Stampings
10.4.1 An austenitic stainless steel nameplate shall be permanently attached to the heat exchanger in
such a manner that it is visible after insulation has been installed.
10.4.2 The nameplate shall be located on the shell, near the channel end.
10.4.3 The following parts shall be stamped with the manufacturer’s serial number:
a)
shell leg;
b)
shell closure flange;
c)
tube closure flange;
d)
return closure;
e)
tubesheets;
f)
test ring flange and gland.
11 Preparation for Shipment
11.1
Protection
11.1.1 All liquids used for cleaning or testing shall be drained from heat exchangers before shipment.
11.1.2 Heat exchangers shall be free from foreign matter prior to shipment.
11.1.3 All openings in heat exchanger units shall be suitably protected to prevent damage and possible
entry of water or other foreign material.
11.1.4 All flange-gasket surfaces shall be coated with an easily removable rust preventative and shall be
protected by suitably attached durable covers of such material as wood, plastic or gasketed steel.
11.1.5 All threaded connections shall be protected by metal plugs or caps of compatible material.
11.1.6 Connections that are beveled for welding shall be suitably covered to protect the bevel from
damage.

11.1.7 The purchaser shall specify if there are requirements for surface preparation and protection (e.g.
painting).
HAIRPIN-TYPE HEAT EXCHANGERS
27
11.1.8 Exposed threads of bolts shall be protected with an easily removable rust preventative to prevent
corrosion during testing, shipping and storage. Tapped holes shall be plugged with grease.

11.1.9 The purchaser shall specify if an inert gas purge and fill is required. Positive pressure shall be
indicated by a pressure gage. Gages shall be suitably protected from damage during transportation. The
purchaser shall maintain the positive pressure of the inert gas during storage.
11.2
Identification
11.2.1 The item number, shipping mass and purchaser’s order number shall be clearly marked on the
heat exchanger.
11.2.2 All boxes, crates or packages shall be identified with the purchaser’s order number and the item
number.
11.2.3 The words “DO NOT WELD” shall be stenciled on the parts of the equipment that have been
postweld heat-treated.
12 Supplemental Requirements
12.1

General
The purchaser shall specify if the additional requirements in Section 12 shall be applied to one or both
sides of the heat exchanger. These supplemental requirements should be considered by the purchaser if
the cylinder thickness of a heat exchanger component exceeds 50 mm (2 in.), or if the service is
considered critical.
12.2
Design
The attachment of welded nozzles and other connections to components shall have integral
reinforcement. The nozzles and other connections shall be attached using full-penetration groove welds
with additional fillet or butt welds. They can be set-on, set-in, or integrally reinforced forging type inserts.
Set-on type connections shall not be welded to plate that contains laminations or other defects and shall
be used only if the component is pipe or forged or if the component plates are ultrasonically examined in
the area of attachment. In this case, the examination for laminations and other defects shall be carried out
for a radial distance of at least twice the thickness of the component.
12.3
Examination
12.3.1 All material for formed heads or cylinders exceeding 50 mm (2 in.) in thickness shall be
ultrasonically examined. Non-destructive examination procedures and acceptance criteria shall comply
with the pressure design code.
12.3.2 All forgings, except standard flanges designed as described in 7.8, shall be ultrasonically
examined in accordance with the pressure design code. Non-destructive examination procedures and
acceptance criteria shall comply with the pressure design code and shall be approved by the purchaser.
12.3.3 For ultrasonic examination of welds, plates and forgings, the purchaser shall be supplied with a
report providing diagrams of the surfaces scanned and indications obtained, the areas repaired, the
nature of defects repaired, and the repair procedures used.
12.3.4 Magnetic-particle examination shall be performed on all pressure-containing plate edges and
openings before welding. Any defects found shall be removed and any necessary repairs performed.
Liquid penetrant examination shall be substituted for nonmagnetic materials.
28
API STANDARD 663
12.3.5 Magnetic-particle examination shall be performed on all pressure-retaining welds and weld
repairs, after PWHT. If accessible, the back side of the root pass shall be examined after being prepared
for final welding. Both sides of accessible completed welds shall be examined. Liquid penetrant
examination shall be substituted for nonmagnetic materials.
12.3.6 Magnetic-particle examination shall be performed on all pressure-boundary attachment welds.
12.3.7 Magnetic-particle examination shall be performed on areas where temporary lugs have been
removed. These areas shall be prepared by grinding them before the examination. Penetrant test can be
substituted.
12.3.8 After the hydrostatic test, a magnetic-particle examination shall be performed on all external
pressure-retaining welds and all internal nozzle welds that are accessible without disassembling the heat
exchanger.
12.3.9 Welds subject to full radiography that cannot be radiographed shall be ultrasonically examined.
12.3.10 Full radiographic examination shall be performed on all pressure-retaining butt welds
12.3.11 Ultrasonic examination shall be performed on all pressure-retaining butt welds [for components
over 50 mm (2 in.) thick] after postweld heat treatment. Ultrasonic examination shall comply with the
pressure design code. The entire volume of deposited weld metal shall be examined from two directions.
Before the welds are examined, the adjacent base material shall be examined by means of longitudinal
beam with a 100 % scan for a distance of twice the plate thickness back from the weld. A diagram shall
be prepared indicating all areas larger than 12 mm (1/2 in.) in diameter that show a loss of back-reflection
of 50 % or more. The acceptance criteria shall be agreed upon by the purchaser and the vendor.
Annex A
(informative)
Recommended Practices
A.1 General
This annex has been prepared to give advice to the designer. The advice is offered for guidance only.
The descriptions and numbers following are those of subsections in the main body of this standard.
A.2 Design
A.2.1 Cyclic Design—Guidance to 7.3
A.2.1.1
The following is guidance to assist in identifying a potential cyclic service application:
⎯ 20 % variance in normal operating pressure; and/or;
⎯ 20 % variance in process flow rate; and/or
⎯ variation in normal operating temperature that exceeds 110 °C (200 °F).
One cycle is where the variance occurs within a time frame of less than 24 h and the number of cycles
exceeds 12 per year.
NOTE
The variation in the normal operating temperature is suggested by API RP 571, Section 4.2.9.3 c),
Thermal Fatigue.
A.2.1.2 For assistance in specifying cyclic conditions, it is suggested that the purchaser follow the
guidance of ASME BPVC, Section VIII, Division 2, and complete a User Design Specification.
Methodologies are also available in other pressure design codes, including EN 13445 (all parts).
A.2.1.3 The vendor can use the screening method provided in ASME BPVC, Section VIII, Division 2, to
determine whether a fatigue analysis is required for the given cyclic loading. If required, rules for
performing a full fatigue analysis are included. Methodologies are also available in other pressure design
codes, including EN 13445 (all parts).
A.3 Fabrication
A.3.1 Heat Treatment—Guidance to 9.4
U-bends formed from tube materials having low ductility or materials that are susceptible to work
hardening can require special consideration. If cold working induces embrittlement or susceptibility to
stress corrosion in some materials or environments, then heat treatment should be considered.
A.4 Inspection and Testing
A.4.1 Quality Assurance—Guidance to 10.1
The purchaser shall specify the required degree of involvement, for example:
a)
verification that qualified welding procedures and qualified welders and welding operators are being
used by the manufacturer;
29
30
API STANDARD 663
b)
verification that the construction complies with the applicable drawings and with this standard;
c)
review and/or examination of the results of any specified nondestructive examination;
d)
witnessing of hydrostatic testing and any additional testing specified by the purchaser;
e)
examination of required material certificates and the manufacturer’s data reports.
A.5 Preparation for Shipment Protection
A.5.1 Protection—Guidance to 11.1
A.5.1.1 If water residues cannot be tolerated, equipment should be dried by one of the following
methods:
a)
blowing dry air or nitrogen, of relative humidity less than 15 % (usually dehumidified), through the
heat exchanger and monitoring the outlet air until the relative humidity falls below 30 %;
b)
evacuating the heat exchanger with a vacuum pump to an absolute pressure between 0.4 kPa
(0.06 psi) and 0.5 kPa (0.075 psi).
A.5.1.2 After draining and drying, internal surfaces can be protected against corrosion by the addition
of a desiccant (e.g. silica gel), by the addition of a volatile corrosion inhibitor, or by blanketing with an inert
gas, such as nitrogen [typically at a gauge pressure of up to 100 kPa (15 psi)].
Annex B
(informative)
Hairpin Heat Exchanger Checklist
The checklist (Table B.1) is used to record the specific requirements the purchaser makes in response to
the sections and subsections in this standard alongside which bullets () are used to indicate that more
information is required or it is necessary to make a decision.
Completion of the checklist is the responsibility of the purchaser.
Table B.1—Checklist for Hairpin Heat Exchangers
Section
Requirement
4.1
Pressure design code.
4.4
Applicable local regulations.
4.7
Specify if the unit subject to sour service.
Item
Define code requirements.
Yes
No
Copies required of applicable welding procedure specifications,
procedure qualifications and weld map.
For
review
For
record
Not
required
6.2.4 a)
Copies required of mechanical design calculations for
nonproprietary pressure-retaining components.
For
review
For
record
Not
required
6.2.4 b)
Minimum required thicknesses for all pressure-retaining
components.
For
review
For
record
Not
required
6.2.4 c)
Copies required of maximum allowable working pressure
calculations.
For
review
For
record
Not
required
6.2.4 d)
Copies required of design calculations based on seismic, wind,
transportation and/or piping loads.
For
review
For
record
Not
required
6.2.4 e)
Copies required of proposed procedures for assembly of flanged
joints and required lubricants.
For
review
For
record
Not
required
6.2.4 f)
Copies required of design calculations for thermal loads imposed on
nozzles of stacked heat exchangers.
For
review
For
record
Not
required
6.2.4 g)
Copies required of flow-induced vibration analysis.
For
review
For
record
Not
required
6.2.4 h)
CMTR for all carbon steel materials in contact with the process fluid.
For
review
For
record
Not
required
6.2.3
6.3
Format and quantities for the listed final documents.
7.1.1
Maximum design temperature and a minimum design metal
temperature (MDMT).
7.3.1
Specify if hot or cold side subject to cyclic service.
7.3.2
If cyclic service is specified, specify the variation, the time for the
variation and the number of cycles or frequency.
7.3.3
If cyclic service is specified, define the type of analysis required.
31
32
API STANDARD 663
Table B.1 (continued)
Requirement
7.7.1.5
Has the hairpin exchanger been selected to mitigate a complete
tube rupture scenario?
7.7.1.6
Is there a maximum allowable length of straight tube? If so specify.
Item
Yes
No
7.8.8
Insulation thickness.
7.8.11
Are chemical cleaning connections required?
Yes
No
7.11.6
Will powered bolt-tensioning or torquing devices be used in the
field?
Clarify if the use is for nozzles and/or girth flanges.
Type of equipment or the required space.
Yes
No
8.2.3
For carbon steel materials in sulfide stress cracking service, the
maximum allowable carbon equivalent shall be agreed to, including
restrictions on other residual elements and micro-alloying elements.
9.3.10
For carbon steel in sour or wet hydrogen sulfide service, specify if
weld procedure qualifications shall include a micro-hardness survey.
Specify any additional restrictions on residual elements or
micro-alloying elements for the qualification test material.
Yes
No
9.4.2
Requirements for heat treatment after bending for the bend portion
of U-tubes.
9.4.4
Is heat treatment required for process reasons?
Yes
No
9.4.5
Is postweld heat treatment required for weld-overlaid components?
Yes
No
10.1.1
Is information on vendor’s quality control system required? Does
this include a quality control plan?
Yes
No
10.2.3
Is it required to hardness test the weld metal of pressure-retaining
welds in carbon steel components?
Yes
No
10.2.14
Is it required that all carbon steel plate be subjected to an ultrasonic
lamination check?
Yes
No
10.3.6
Any additional requirements for equipment drying or preservation.
11.1.7
Any additional requirements for surface preparation and protection.
11.1.9
Is an inert gas purge and fill required?
Yes
No
12.1
Are the additional requirements specified in Section 12 required? If
so, shall they be applied to one or both sides of the heat
exchanger?
--`,,``````,````,,```,`,,,`,,`,-`-`,,`,,`,`,,`---
Section
Annex C
(informative)
Hairpin Heat Exchanger Datasheets
The following datasheets are provided to assist designers, vendors and purchasers in specifying the data
necessary for the design of hairpin heat exchangers for petroleum, petrochemical and natural gas
services. Entries that are not relevant to hairpin exchangers should be annotated as “N/A.”
Completion of the datasheet is a joint responsibility of the purchaser and vendor. The purchaser (owner
or contractor) is responsible for the process data, which define the purchaser’s explicit requirements.
After the exchanger has been fabricated, the vendor should complete the datasheets to make a
permanent record that accurately describes the equipment “as-built”.
Additional datasheets may be required to define the hairpin heat exchanger and examples are included in
Figure C.1 and Figure C.2.
⎯ Connection schedule (see page 2 of Figure C.1 and Figure C.2), materials of construction (see
page 2 of Figure C.1 and Figure C.2); gaskets (see page 2 of Figure C.1 and Figure C.2). These are
used if the designer/user requires such level of detail to define materials for individual components.
These sections may not be necessary if page 1 defines the information sufficiently.
⎯ Additional remarks, sketches, etc. (see page 3 of Figure C.1 and Figure C.2). These are used for
additional remarks if sufficient space is not available on page 1 and also for schematic sketches to
illustrate required features of the design and tube layouts, if necessary, to provide this information to
the manufacturer.
⎯ Additional process information (see page 4 of Figure C.1 and Figure C.2). One or two pages can be
necessary if boiling and/or condensing fluids with ranges of physical properties occur.
⎯ Additional cyclic service design data (see page 5 of Figure C.1 and Figure C.2). This is required only
for exchangers where the unit is subject to cyclic service.
33
34
API STANDARD 663
Co mpany
Engineering co ntracto r
HAIRPIN HEAT EXCHANGER
DATA SHEET (SI UNITS)
P.O. No.:
Doc. No.:
Page 1 of
1 Client:
Location:
2 Process unit:
Item No.:
3 Job No.:
Fabricator:
4 Service of unit:
No. of units:
double-pipe/multi-tube
Connected in:
m2
Sections/unit:
5 Size:
Type:
6 Total effective heat transfer area (plain/finned):
Parallel
Series
Effective heat transfer area per section:
Shell side
7 Perform ance of one unit
8
Inlet
m2
Tube side
Outlet
Inlet
Outlet
9 Fluid name:
10 Fluid quantity, total:
kg/h
11
Vapour (relative molecular mass):
kg/h
12
Liquid:
kg/h
13
Steam:
kg/h
14
Water:
kg/h
15
Non-condensable (relative molecular mass):
kg/h
16 Temperature:
/
/
@
@
/
/
°C
17 Density (vapour/liquid):
kg/m3
18 Viscosity (vapour/liquid):
mPa·s
19 Specific heat (vapour/liquid):
kJ/(kg·K)
20 Thermal conductivity (vapour/liquid):
W/(m·K)
21 Specific latent heat:
kJ/kg @ °C
22 Inlet pressure:
kPa (ga)
23 Velocity:
m/s
24 Pressure drop (allow able/calculated):
kPa
25 Fouling resistance:
m2·K/W
26 Average film coefficient:
W/(m2·K)
27 Heat exchanged:
kW
W/(m2·K)
kg/(m·s 2)
28 Heat transfer rate:
29 Rho-V 2:
Mean temperature difference (MTD):
Required:
Inlet nozzle:
°C
Fouled:
Bundle entrance:
Clean:
Bundle exit:
30 Construction per unit
31 Tube number:
32 Tube type:
OD:
Plain/Finned
33 Tube w all thickness:
mm
34 Tube pitch:
mm
35 Tube length:
mm
Fin type:
Nozzles – Number, size and rating
Long./Other
minimum w all/average w all
m
Tube layout:
Outlet:
Tube type: plain/finned/other
Intermediate:
36 Tube to tubesheet joint:
37 Shell diameter:
Tube side
/
/
Vent:
mm
(ID/OD)
/
Drain:
38 Cross-baffle type:
Pressure relief:
39 Baffle spacing: c/c
40 Baffle cut:
mm
No. of cross passes:
%
vertical/horizontal
41 Tube support type:
--`,,``````,````,,```,`,,,`,,`,-`-`,,`,,`,`,,`---
Shell side
Inlet:
42 Tube closure type:
43 Impingement protection:
Design pressure:
Spacing: c/c
mm
Standard/Separate Head/Rod Through/Welded
(Y/N)
Type:
kPa (ga)
Vacuum:
kPa (abs)
Design temp. (Max/MDMT):
Corrosion allow ance:
°C
mm
44 Materials of construction
45 Shell:
Tubes:
Gaskets
46 Return bend housing:
Shell side:
47 Channel:
Tube side:
48 Front closure:
Spare gaskets required:
49 Rear closure:
50 Tubesheet:
Insulation - shell:
mm
51 Shell end flange:
Insulation - channel:
mm
52 Compression/Tube fitting flanges:
53 Sealing rings
Splitting rings:
54 Baffles:
55 Tube supports:
56 Pressure design code:
57 Remarks/sketch:
Stamp:
Calculate MAWP:
(Y/N)
TEMA Class:
58
59
60
Rev. No.
Description
Date
Prepared by
Review ed by
inlet/outlet
35
HAIRPIN-TYPE HEAT EXCHANGERS
--`,,``````,````,,```,`,,,`,,`,-`-`,,`,,`,`,,`---
36
API STANDARD 663
HAIRPIN-TYPE HEAT EXCHANGERS
37
38
API STANDARD 663
HAIRPIN-TYPE HEAT EXCHANGERS
39
40
API STANDARD 663
HAIRPIN-TYPE HEAT EXCHANGERS
41
42
API STANDARD 663
HAIRPIN-TYPE HEAT EXCHANGERS
43
Bibliography
[1]
EN 10160 4 , Ultrasonic testing of steel flat product of thickness equal or greater than 6 mm
(reflection method)
[2]
EN 13445 (all parts), Unfired pressure vessels
[3]
ASME Boiler and Pressure Vessel Code (BPVC), Section VIII, Rules for construction of pressure
vessels
[4]
ASME Boiler and Pressure Vessel Code (BPVC), Section VIII, Rules for construction of pressure
vessels, Division 2, Alternative Rules
[5]
ASME B16.11, Forged Fittings, Socket-Welding and Threaded
[6]
ASME B1.20.1, Pipe Threads, General Purpose (Inch)
[7]
WRC 537 5, Local Stresses in Spherical and Cylindrical Shells Due To External Loading
[8]
ASTM B359/B359M, Standard Specification for Copper and Copper-Alloy Seamless Condenser
and Heat Exchanger Tubes with Integral Fins
[9]
API Recommended Practice 571, Damage Mechanisms Affecting Fixed Equipment in The
Refining Industry
[10]
ASME SA-578, Specification for Straight-Beam Ultrasonic Examination of Plain and Clad Steel
Plates for Special Applications
4
European Committee for Standardization, Avenue Marnix 17, B-1000, Brussels, Belgium, www.cen.eu.
The Welding Research Council, 3 Park Avenue, 27th Floor, New York,
New York 10016-5902,
www.forengineers.org.
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